Investigations and analysis of flow phenomena of secondary motions in axial flow inducers Progress report, nine month period ending 31 Mar. 1969
Flow measurements of secondary motions in axial flow impellers
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Flow measurements of secondary motions in axial flow impellers
Flow field and drag characteristics of several laminar boundary layer tripping element in hypersonic flow
Flow and heat transfer measurements for heated air in subsonic flow through contraction section connecting tube to conical section
Mass flow rates for nearly free molecular flow through two dimensional slit for several tank pressure ratios
Fixed position pressure probe for measuring subsonic flow direction over range of Reynolds number, Mach number and flow angle
Flow liner eliminates high-cycle fatigue in ducts carrying cryogenic fluids. It is capable of handling two-directional, high-velocity cryogenic liquid flow with a 3-inch axial motion without binding within a 25-inch length.
Studies of the properties of five metals with varying tube-wall thickness, with or without and internal coating of trifluorochloroethylene polymer, show that wall characteristics influence flow stability, affect heat transfer coefficients, and influence the transition point from dry- to wet-wall flow.
Calculation of natural gas flow through critical flow nozzles
Approximation for distribution of flow properties in angle of attack plane of conical flows
Mass flow rate calculation of methane and natural gas mixtures through critical flow nozzles
Polymeric materials flow at tube entrance, discussing pressure drop and flow birefringent patterns at tapered and sharp entrances
Simulating downstream flow blockage doors in bypass air duct of turbofan engine with axial flow fan rotor
Flow-induced vibration of bellows with internal cryogenic fluid flows
Equations for mass flow of methane and natural gas mixtures through critical flow nozzles, including real gas effects
Computer program to generate turbine aerodynamic requirements, approximate external blade geometries, and coolant flow requirements for two stage axial flow turbine
Effect of inlet conditions on flow and containment characteristics of coaxial flows for gas core nuclear rockets
Development of flow measuring apparatus for determining low flow performance of resistojet thruster is discussed. Diagram of test equipment is presented. Operation of test equipment is described and numerical relationships are explained.
An analytical solution for the compressible one-dimensional flow in convergent and divergent ducts with friction is obtained. It is found that a nondimensional parameter, N, can be formed using the friction factor, duct half-angle and the ratio of specific heats of the gas. Seven flow regimes are describable with the solution, based on certain bounds on the magnitude of N. The regimes are discussed and corollary data are presented graphically.